Continuous Gust Response and Sensitivity Derivatives Using State-Space Models
暂无分享,去创建一个
[1] Mordechay Karpel,et al. Multidisciplinary optimization of aeroservoelastic systems using reduced-size models , 1992 .
[2] M. Karpel. Size-reduction techniques for the determination of efficient aeroservoelastic models , 1992 .
[3] Mordechay Karpel,et al. Application of aeroservoelastic modeling using minimum-state unsteady aerodynamic approximations , 1991 .
[4] Mordechay Karpel,et al. Time-domain aeroservoelastic modeling using weighted unsteady aerodynamic forces , 1990 .
[5] Peretz P. Friedmann,et al. Towards integrated multidisciplinary synthesis of actively controlled fiber composite wings , 1990 .
[6] M. Karpel,et al. Sensitivity derivatives of flutter characteristics and stability margins for aeroservoelastic design , 1989 .
[7] J. R. Newsom,et al. A method for obtaining reduced-order control laws for high-order systems using optimization techniques , 1981 .
[8] Mordechay Karpel,et al. Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling , 1980 .
[9] Arthur E. Bryson,et al. Applied Optimal Control , 1969 .